Dual-Mode Scramjet Flameholding Operability Measurements

Measurements were made in a direct-connect combustor facility designed to simulate cavity flameholding in a hydrocarbon-fueled dual-mode scramjet combustor where the presence of a shock train upstream of the flameholder has a significant impact on the inlet flow to the combustor and on flameholding...

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Veröffentlicht in:	Journal of propulsion and power 2014-05, Vol.30 (3), p.592-603
1. Verfasser:	Donohue, James M
Format:	Artikel
Sprache:	eng
Schlagworte:	Air temperature Blowouts Combustion chambers Ethylene Flow velocity Fuel injection Fuels Holes Inlet flow Inlet nozzles Inlets Mach number Scramjets Supersonic combustion ramjet engines Test facilities Throttles Trains Upstream
Online-Zugang:	Volltext
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